CN106516083A - 一种小型固定翼无人机的翼梢小翼转动装置 - Google Patents
一种小型固定翼无人机的翼梢小翼转动装置 Download PDFInfo
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- CN106516083A CN106516083A CN201610643365.5A CN201610643365A CN106516083A CN 106516083 A CN106516083 A CN 106516083A CN 201610643365 A CN201610643365 A CN 201610643365A CN 106516083 A CN106516083 A CN 106516083A
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- winglet
- unmanned aerial
- aerial vehicle
- wing
- wingtip
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
Description
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610643365.5A CN106516083A (zh) | 2016-08-01 | 2016-08-01 | 一种小型固定翼无人机的翼梢小翼转动装置 |
Applications Claiming Priority (1)
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CN201610643365.5A CN106516083A (zh) | 2016-08-01 | 2016-08-01 | 一种小型固定翼无人机的翼梢小翼转动装置 |
Publications (1)
Publication Number | Publication Date |
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CN106516083A true CN106516083A (zh) | 2017-03-22 |
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CN201610643365.5A Pending CN106516083A (zh) | 2016-08-01 | 2016-08-01 | 一种小型固定翼无人机的翼梢小翼转动装置 |
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CN (1) | CN106516083A (zh) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108454822A (zh) * | 2018-04-28 | 2018-08-28 | 成都航空职业技术学院 | 一种可拆换小翼装置及其拆换方法 |
CN108945481A (zh) * | 2018-09-17 | 2018-12-07 | 昆明鞘翼科技有限公司 | 一种在板翼下方安装驱动机构增强升力并实现垂直起降的方法 |
CN111017191A (zh) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | 一种翼梢小翼 |
CN111645849A (zh) * | 2020-05-22 | 2020-09-11 | 中国商用飞机有限责任公司 | 一种用于致动和控制飞行器机翼的可折叠翼梢的***和方法 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100051741A1 (en) * | 2008-09-03 | 2010-03-04 | Anvar Ismailov | Unmanned air vehicle |
CN102407938A (zh) * | 2011-10-19 | 2012-04-11 | 南京航空航天大学 | 安装变体翼梢小翼的机翼及其工作方式 |
CN202279235U (zh) * | 2011-09-06 | 2012-06-20 | 成都飞机设计研究所 | 变体鸭式无尾气动布局 |
CN103287578A (zh) * | 2012-03-01 | 2013-09-11 | 贵州帝三数字技术有限公司 | 一种微型通用无人飞行器 |
CN103600835A (zh) * | 2013-11-29 | 2014-02-26 | 石家庄飞机工业有限责任公司 | 一种仿生飞翼无人机的气动外形 |
CN105438441A (zh) * | 2015-12-04 | 2016-03-30 | 中国航天空气动力技术研究院 | 一种翼梢小翼装置 |
CN206107551U (zh) * | 2016-08-01 | 2017-04-19 | 西北农林科技大学 | 一种小型固定翼无人机的翼梢小翼转动装置 |
-
2016
- 2016-08-01 CN CN201610643365.5A patent/CN106516083A/zh active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100051741A1 (en) * | 2008-09-03 | 2010-03-04 | Anvar Ismailov | Unmanned air vehicle |
CN202279235U (zh) * | 2011-09-06 | 2012-06-20 | 成都飞机设计研究所 | 变体鸭式无尾气动布局 |
CN102407938A (zh) * | 2011-10-19 | 2012-04-11 | 南京航空航天大学 | 安装变体翼梢小翼的机翼及其工作方式 |
CN103287578A (zh) * | 2012-03-01 | 2013-09-11 | 贵州帝三数字技术有限公司 | 一种微型通用无人飞行器 |
CN103600835A (zh) * | 2013-11-29 | 2014-02-26 | 石家庄飞机工业有限责任公司 | 一种仿生飞翼无人机的气动外形 |
CN105438441A (zh) * | 2015-12-04 | 2016-03-30 | 中国航天空气动力技术研究院 | 一种翼梢小翼装置 |
CN206107551U (zh) * | 2016-08-01 | 2017-04-19 | 西北农林科技大学 | 一种小型固定翼无人机的翼梢小翼转动装置 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108454822A (zh) * | 2018-04-28 | 2018-08-28 | 成都航空职业技术学院 | 一种可拆换小翼装置及其拆换方法 |
CN108945481A (zh) * | 2018-09-17 | 2018-12-07 | 昆明鞘翼科技有限公司 | 一种在板翼下方安装驱动机构增强升力并实现垂直起降的方法 |
CN111017191A (zh) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | 一种翼梢小翼 |
CN111645849A (zh) * | 2020-05-22 | 2020-09-11 | 中国商用飞机有限责任公司 | 一种用于致动和控制飞行器机翼的可折叠翼梢的***和方法 |
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SE01 | Entry into force of request for substantive examination | ||
CB03 | Change of inventor or designer information | ||
CB03 | Change of inventor or designer information |
Inventor after: Han Wenting Inventor after: Shi Zhiqiang Inventor after: Shao Guomin Inventor after: Liu Junlong Inventor after: Dan Xiujia Inventor after: Zhang Liyuan Inventor before: Shi Zhiqiang Inventor before: Han Wenting Inventor before: Shao Guomin Inventor before: Liu Junlong Inventor before: Dan Xiujia Inventor before: Zhang Liyuan |
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WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170322 |